Limbach L 2400 DT/ET Engine – turbocharged | 96kW (130HP) at 3000rpm | Liquid Cooled Cylinderheads

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Description

Versatile and Efficient, The Advanced Design of the Limbach L 2400 DT/ET Engine – turbocharged

The Limbach L 2400 DT/ETย  is a high-performance, four-cylinder, horizontally opposed engine featuring liquid-cooled cylinder heads, electronic fuel injection, and automatic altitude compensation. Designed for UAVs and light aircraft, it offers smooth and powerful performance with efficient fuel consumption. This UAV Engineย model includes dual ignition, enhancing reliability and performance in demanding conditions.

Key Specifications:
  • Maximum Power: 96 kW (130 HP) at 3000 RPM, providing robust performance for various applications
  • Engine Type: Four-cylinder, horizontally opposed, with liquid-cooled cylinder heads, wet sump pressure lubrication, and electronic engine management
  • Bore and Stroke: 97 mm (3.82 in) bore and 82 mm (3.23 in) stroke
  • Displacement: 2424 cmยณ (147.91 cubic inches)
  • Compression Ratio: 8:1 for a balanced combination of power and fuel efficiency
  • Ignition System: Electronic engine management with variable, memory-mapped firing point (dual ignition on DT model)
  • Spark Plugs: NGK DCPR 7 E with 0.7 mm electrode gap
  • Firing Order: 1 – 3 – 2 – 4, providing balanced operation and reduced vibration
  • Fuel Injection: 4 x Weber injectors for precise fuel management
  • Fuel Requirements: 98 RON unleaded gasoline or AVGAS 100 LL
  • Fuel Pump: Dual electric fuel pumps at 2.5 bar each
  • Starter: 12V, 1.0 kW with solenoid for reliable starting
  • Generator: 14V, 55A to support electrical requirements
  • Oil System: Maximum oil pressure of 7 bar, minimum 1 bar at 2500 RPM, with a 3.5-liter oil capacity
  • Cooling System: Max coolant temperature of 110ยฐC, with an approximate 3-liter coolant capacity
  • Propeller Drive: Direct, anti-clockwise rotation, suitable for variable pitch propellers
  • Dry Weight: 86 kg (excluding accessories)
  • Fuel Consumption: 255 g/kWh at Wide Open Throttle (WOT) and 240 g/kWh at part throttle for efficient fuel use
The L2400 DT/ET engineโ€™s combination of liquid cooling, advanced electronic controls, and dual ignition (on DT) make it a powerful and efficient choice for high-altitude and demanding aerial applications, with reliable performance and flexibility to meet diverse operational needs.

 

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For a comprehensive reading of related products, please visit the Motionew website.

Specifications

Specifications of Limbach Engineย L 2400 DT/ET

Maximum Power 96 kW / 130 HP at 3000 rpm
Bore 97 mm / 3.82 inch
Stroke 82 mm / 3.23 inch
Displacement 2424 cm3 / 147.91 cub. in.
Compression ratio 8 : 1
Ignition Electronic engine management
Spark plugs NGK DCPR 7 E
Electrode spacing 0.7 mm
Firing Order 1 – 3 – 2 – 4
Firing point variable, memory mapped
Injectors 4 x Weber
Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL
Air cleaner LIMBACH
Fuel pump 2 x electric 2.5 bar
Starter with solenoid 12 V – 1.0 kW
Generator 14 V – 55 A
Oil pressure max. 7 bar; min. 1 bar at 2500 rpm
Oil temperature max. 120 ยฐC; min. 50 ยฐC
Oil capacity 3.5 Itrs
Coolant temperature max. 110 ยฐC
Coolant capacity approx. 3 ltrs
Tachometer drive electric signal
Propeller drive direct, anti-clockwise
Propeller hub for variable pitch propeller
Dry weight 86 kg, plus accessories
Fuel consumption 255 g/kWh at WOT
240 g/kWh at part throttle

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